Mean pressure gradient effects on the performance of ramjet cavity stabilized flames-Reference-Cited by-同舟云学术

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Mean pressure gradient effects on the performance of ramjet cavity stabilized flames

Published:2023-10 Issue: Volume:141 Page:108533
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Morales Anthony J.,Smerina David M.^ORCID,Thornton Mason.R.,Rising Cal J.^ORCID,Sosa Jonathan,Johnson Ryan F.,Kessler David A.,Goodwin Gabriel,Ahmed Kareem A.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference82 articles.

1. Hypersonic flight and the Re-entry problem;Turner;Aeronaut. Sci.,1958

2. Stabilized detonation for hypersonic propulsion;Rosato;Proc. Natl. Acad. Sci. USA,2021

3. Combined-cycle engines;Kanda;Encycl. Aerosp. Eng.,2010

4. Flame propagation and stabilization in dual-mode scramjet combustors: a survey;Huang;Prog. Aerosp. Sci.,2018

5. Cavity-based flameholding for chemically-reacting supersonic flows;Barnes;Prog. Aerosp. Sci.,2015

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Flame Induced Vortex Dynamics in Cavity Stabilized Combustion;AIAA SCITECH 2024 Forum;2024-01-04

2. Non-periodic shear layer instabilities driving local extinction in premixed ramjet cavity flames;Proceedings of the Combustion Institute;2024

3. Numerical Investigation of the Distributed Combustion In the Thermal Choked Solid Fuel Combined Cycle Engine;2024

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